Basic Information

Category Helicopter Type Transport
Year Commissioned 2002 Year Decommissioned 0
Agility 1 Damage Points (DP) 5
Empty Weight 10615 kg Max Weight 22668 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Medium Aircraft (12.1-18m)
Cost 0 Hypothetical No
Payload Weight 10886 kg Crew 3 people

Aircraft Capabilities

Nap-of-the-Earth (NOE) Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles)

Sensor Parameters

Model Purpose Range Scan Interval Generation
AN/APR-39A(V)1 RWR, Radar Warning Receiver 0.00 - 120.00 nm 5 sec Late 1980s
AN/ALQ-156 MAWS, Missile Approach Warning System 0.00 - 5.00 nm 60 sec Early 1980s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
AN/APR-39A(V)1 SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2
AN/ALQ-156 SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
Trooper   x 33
Trooper   x 55

Signatures

Type Front Side Rear
Visual Detection Range 2.06 nm 6.14 nm 2.06 nm
Visual Classification Range 1.21 nm 3.47 nm 1.89 nm
Infrared Detection Range 2.06 nm 7.92 nm 11.35 nm
Infrared Classification Range 1.21 nm 3.47 nm 1.21 nm
Radar, A-D Band (30-2000 MHz) 2.2 dBsm (1.66 m²) 4.6 dBsm (2.88 m²) 2.2 dBsm (1.66 m²)
Radar, E-M Band (2-100 GHz) 2.2 dBsm (1.66 m²) 4.6 dBsm (2.88 m²) 2.2 dBsm (1.66 m²)

Default Configuration

Model Comments
M-130 x 2 [60 Cartridges] Chaff & Flare Dispenser

Datalink

Type Model Range Channels
Radio VHF Radio [Unsecure] 100 nm 0
Radio UHF Radio [Unsecure] 100 nm 0

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
2x T55-L-714A Helo Turboshaft 2 4867 - 0.503 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 6260